Electrical control system for actuating inboard spoilers on airc

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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Details

244 90R, 244113, 244213, B64C 1304, B64C 1350

Patent

active

040870650

ABSTRACT:
An electrical system for actuating the inboard spoilers on the wings of an aircraft in response to the lateral control input from the pilot control wheel and to the position of the pilot speed brake lever. The pilot speed brake lever position signal being used to select the modulation provided by a three mode function generator which generates the signal that actuates the spoilers.

REFERENCES:
patent: 3618880 (1971-11-01), Hagaman et al.

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